Computation of the roll characteristics of a finned projectile

Journal of Spacecraft and Rockets

Volumn 33, Issue 6, 1996, Pages 769-775

  Weinacht, Paul ^a,b,c   Sturek, Walter B ^a,c,d  

^a U S ARMY RESEARCH LABORATORY   (United States)

^b Weapons Technology Directorate

^c AIAA ^*

^d Adv Simulat High Perf Comp D

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; COMPUTATIONAL METHODS; DAMPING; ESTIMATION; FLIGHT DYNAMICS; NAVIER STOKES EQUATIONS;

CENTRIFUGAL ACCELERATION; CORIOLIS ACCELERATION; FINNED PROJECTILES; RANGE FIRINGS; ROLL CHARACTERISTICS;

PROJECTILES;

EID: 0030290410     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/3.26836     Document Type: Article

References (15)

1. Wardlaw, A. B., Jr., Priolo, F. J., and Solomon, J. M., "Multiple-Zone Strategy for Supersonic Missiles," Journal of Spacecraft and Rackets, Vol. 24, No. 4, 1987, pp. 377-384.
2. Oberkampf, W. L., "Prediction of Roll Moments on Finned Bodies in Supersonic Flow," Journal of Spacecraft and Rockets, Vol. 12, No. 1, 1975, pp. 17-21.
3. Prakash, S., and Khurana, D. D., "A Simple Estimation Procedure of Roll-Rate Derivatives for Finned Vehicles," Journal of Spacecraft and Rockets, Vol. 21, No. 3, 1984, pp. 318-320.
4. Eastman, D. W., "Roll Damping of Cruciform-Tailed Missiles," Journal of Spacecraft and Rockets, Vol. 23, No. 1, 1986, pp. 119, 120.
5. Mikhail, A. G., "Roll Damping for Projectiles Including Wraparound, Offset, and Arbitrary Number of Fins," Journal of Spacecraft and Rockets, Vol. 32, No. 6, 1995, pp. 929-937.
6. Devan, L., "Nonaxisymmetric Body, Supersonic, Inviscid Dynamic Derivative Prediction," Proceedings of the AIAA 7th Applied Aerodynamics Conference, AIAA, Washington, DC, 1989 (AIAA Paper 89-2195).
7. Murphy, C. H., "Free Flight Motion of Symmetric Missiles," U.S. Army Ballistic Research Lab., Rept. 1216, Aberdeen Proving Ground, MD, July 1963, pp. 18-21.
8. Schiff, L. B., and Steger, J. L., "Numerical Simulation of Steady Supersonic Viscous Flow," AIAA Journal, Vol. 18, No. 12, 1980, pp. 1421-1430.
9. Baldwin, B. S., and Lomax, H., "Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows," AIAA Paper 78-257, Jan. 1978.
10. Beam, R., and Warming, R. F., "An Implicit Factored Scheme for the Compressible Navier-Stokes Equations," AIAA Journal, Vol. 16, No. 4, 1978, pp. 85-129.
11. Rai, M. M., and Chaussee, D. S., "New Implicit Boundary Procedure: Theory and Applications," AIAA Paper 83-0123, Jan. 1983.
12. Rai, M. M., Chaussee, D. S., and Rizk, Y. M., "Calculation of Viscous Supersonic Flows over Finned Bodies," AIAA Paper 83-1667, July 1983.
13. Nielsen, J. N., Missile Aerodynamics, McGraw-Hill, New York, 1960, pp. 15, 16.
14. Liepmann, H. W., and Roshko, A., Elements of Gasdynamics, Wiley, New York, 1957, pp. 109-113.
15. Brandon, F. J., private communication, U.S. Army Ballistic Research Lab., Aberdeen Proving Ground, MD, Jan. 1989.